An Investigation Of The Interference Effects Of A Sting Support System On The Pressure Distribution Over A Body Of Revolution
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Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1991
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with Aeronautics categories.
An Investigation Of The Interference Effects Of A Sting Support System On The Pressure Distribution Over A Body Of Revolution
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Author : Harris M. Schurmeier
language : en
Publisher:
Release Date : 1949
An Investigation Of The Interference Effects Of A Sting Support System On The Pressure Distribution Over A Body Of Revolution written by Harris M. Schurmeier and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Electronic dissertations categories.
Recent Progress In Some Aircraft Technologies
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Author : Ramesh K. Agarwal
language : en
Publisher: BoD – Books on Demand
Release Date : 2016-09-08
Recent Progress In Some Aircraft Technologies written by Ramesh K. Agarwal and has been published by BoD – Books on Demand this book supported file pdf, txt, epub, kindle and other format this book has been release on 2016-09-08 with Technology & Engineering categories.
The book describes the recent progress in some engine technologies and active flow control and morphing technologies and in topics related to aeroacoustics and aircraft controllers. Both the researchers and students should find the material useful in their work.
Investigation Of The Drag Of Various Axially Symmetric Nose Shapes Of Fineness Ratio 3 For Mach Numbers From 1 24 To 7 4
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Author : C. H. Wilts
language : en
Publisher:
Release Date : 1958
Investigation Of The Drag Of Various Axially Symmetric Nose Shapes Of Fineness Ratio 3 For Mach Numbers From 1 24 To 7 4 written by C. H. Wilts and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aeronautics categories.
U S Government Research Development Reports
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Author :
language : en
Publisher:
Release Date : 1970
U S Government Research Development Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Science categories.
An Experimental Investigation Of Support Interference On A Blunt Body Of Revolution At A Mach Number Of Approximately 20
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Author : Charles George Miller
language : en
Publisher:
Release Date : 1965
An Experimental Investigation Of Support Interference On A Blunt Body Of Revolution At A Mach Number Of Approximately 20 written by Charles George Miller and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Interference (Aerodynamics) categories.
Sting Interference Effects As Determined By Measurements Of Dynamic Stability Derivatives Surface Pressure And Base Pressure For Mach Numbers 2 Through 8
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Author : Bob L. Uselton
language : en
Publisher:
Release Date : 1980
Sting Interference Effects As Determined By Measurements Of Dynamic Stability Derivatives Surface Pressure And Base Pressure For Mach Numbers 2 Through 8 written by Bob L. Uselton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Hypersonic wind tunnels categories.
Wind tunnel tests were conducted to provide support interference information for planning and directing wind tunnel tests at supersonic and hypersonic Mach numbers. Sting-length and sting-diameter effects on base and surface pressures of a blunt 6-deg cone with a sliced base were investigated at Mach numbers 2, 3, 5, and 8. Dynamic stability tests on a blunt 7-deg cone were also conducted at Mach numbers 2, 5, and 8. The objectives of the 7-deg cone tests were to define critical sting lengths as determined by the measurement of dynamic stability derivatives, static pitching moment, and base pressure. Two frequencies of oscillation were investigated, and data were obtained for laminar, transitional, and turbulent boundary-layer conditions at the model base. The data from the 6- and 7-deg cone tests showed that the critical sting length depended on the interference indicator, Mach number, angle of attack, state of the model boundary layer, and frequency of oscillation. The critical sting length was generally less for models with turbulent boundary layers than for those with laminar boundary layers. A critical sting length of 2.5 model diameters was determined to be suitable for all test conditions that produced a turbulent boundary layer at or ahead of the model base.
Report
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Author :
language : en
Publisher:
Release Date : 1958
Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aeronautics categories.
Some Effects Of Nose Bluntness And Fineness Ration On The Static Longitudinal Aerodynamic Characteristics Of Bodies Of Revolution At Bussonic Speeds
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Author : William C. Hayes
language : en
Publisher:
Release Date : 1961
Some Effects Of Nose Bluntness And Fineness Ration On The Static Longitudinal Aerodynamic Characteristics Of Bodies Of Revolution At Bussonic Speeds written by William C. Hayes and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics categories.
Annual Report Of The National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :
Annual Report Of The National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Aeronautics categories.